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Wind-tunnel investigation of Saturn S-IC AERODYNAMIC engine gimbal forces and base pressures using a cold-flow-jet simulation techniqueAerodynamic hinge moments for scale model boost stage nozzle of Saturn V launch vehicle during cold flow jet simulation
Document ID
19670030895
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Blaha, B. J. (NASA Lewis Research Center Cleveland, OH, United States)
Bresnahan, D. L. (NASA Lewis Research Center Cleveland, OH, United States)
Wasko, R. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1967
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-1470
Report Number: NASA-TM-X-1470
Accession Number
67N40224
Funding Number(s)
CONTRACT_GRANT: 128-31-11-03-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HINGE MOMENT
SATURN V LAUNCH VEHICLE
AERODYNAMIC CHARACTERISTICS
ROCKET NOZZLE

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